{"created":"2023-06-20T15:10:02.543428+00:00","id":39640,"links":{},"metadata":{"_buckets":{"deposit":"36e38296-d70a-4845-9f7c-51c97e39ab32"},"_deposit":{"created_by":1,"id":"39640","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39640"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039640","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443712","443711"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ウインドシア中の航空機離陸および着陸に対する逆ダイナミックス制御"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"11","bibliographicPageStart":"1","bibliographicVolumeNumber":"1274T","bibliographic_titles":[{},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告は、ウィンドシア中を飛行する航空機の制御について述べる。逆ダイナミックス法を用いて、最低速度に対する制限のもとで地面に対する設定径路を維持するための制御則を、離陸および着陸の各々の場合について構築し、6自由度を持つ飛行シミュレータを用いて異なるウィンドシアおよび異なる飛行条件に対するシミュレーション試験を行った。その結果、ウィンドシア中においても、制御対象の航空機は安全に離陸でき、着陸時にはほぼ設定径路を維持できることが分かった。さらに、設計された制御則は、ウィンドシアによる外乱および飛行条件の変化によるモデルパラメータの変動の双方に対してロバスト性を持つことが示された。また、ウィンドシア遭遇時における、パイロットによる手動操縦と本報告に示した制御則による自動操縦の違いも示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper is concerned with the guidance of an aircraft flight in the presence of windshear. Based on following a nominal approach path relative to the ground, and subject to a minimum airspeed constraint, two guidance laws are synthesized by inverse dynamics technique for take off and landing respectively. Simulation tests are performed in a six degree-of-freedom flight simulator for different windshear histories and different flight conditions, these results illustrate that the controlled aircraft could take off safely and follow the nominal landing path approximately in windshear, and the designed robust controllers are insensitive to both external windshear disturbance and the model parameters variation with change in flight conditions. The different results between manual operation and autopilot control for against windshear are also compared.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000011000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1274T","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 飛行実験部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Wang, L."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wang, Lixin","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr1274t.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1274t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39640/files/naltr1274t.pdf"},"version_id":"56f27061-6430-477f-9bb3-5bea459a4d41"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ウインドシア","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行制御","subitem_subject_scheme":"Other"},{"subitem_subject":"逆ダイナミックス制御","subitem_subject_scheme":"Other"},{"subitem_subject":"設定経路","subitem_subject_scheme":"Other"},{"subitem_subject":"離陸","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"6自由度","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行条件","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション研究","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行安全","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"外乱","subitem_subject_scheme":"Other"},{"subitem_subject":"パラメータ変動","subitem_subject_scheme":"Other"},{"subitem_subject":"ロバスト性","subitem_subject_scheme":"Other"},{"subitem_subject":"windshear","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse dynamics control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nominal approach path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"take off","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"six degree of freedom","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation research","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight safety","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parameter variation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robustness","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Inverse dynamics control for aircraft take off and landing in windshear","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Inverse dynamics control for aircraft take off and landing in windshear","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39640","relation_version_is_last":true,"title":["Inverse dynamics control for aircraft take off and landing in windshear"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:20:02.785647+00:00"}